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Course description A320 CFM or V2500
Engine Run-up Initial Training.doc
30/01/2009
WE QUALIFY!
PART-147 APPROVED TRAINING CENTER
19, rue Marcel ISSARTIER
Bât. M5 RDC – Station 57
CS 50008 - 33693 Mérignac Cedex - France
Phone : +33 (0)5 56 55 41 63
Fax : +33 (0)5 56 55 44 68
Site : www.sabenatechnicstraining.com
Email : training@sabenatechnics.com
SIREN 452 506 793 - VAT FR 97 452 506 793
R.C.S. Bordeaux 452 506 793
1 / 2
A318/A319/A320/A321 CFM Engine Run-up
A319/A320/A321 V2500 Engine Run-up
Initial Training
Course Description
Duration 3-4 Days
(depending on simulator availability), divided as follows:
- 1 theoretical day
- 1 simulator session for 4 trainees : 1 briefing hour + 4 hours + 1 debriefing hour
- 1-2 additional simulator sessions : 1 briefing hour + 4 hours + 1 debriefing hour
Objectives Upon completion of this course the trainee shall:
• be able to safely operate the engine after a major repair and/or replacement of engine components
• identify normal and abnormal start procedures
• carry out power plants tests in accordance with the Maintenance Manual for the according engine installed
on the Airbus aircraft in question
Course capacity Standard class: 4 trainees
Target
population
Technical personnel associated with line and/or base/heavy maintenance activities requiring authorization for
engine run-up.
Prerequisite Personnel must be qualified on the according Airbus aircraft equipped with the relevant engines as Aviation
Maintenance Technician (AMT).
Participants should have 6 month recent practical experience on this aircraft (or equivalent type) or engine run
up certification on other aircraft type. In addition, they should have a basic active knowledge of theoretical ATA
chapters (24, 26, 31, 70 – 80)
Students should be able to read, write and communicate at an understandable level in English language.
Language English / French
Course location According to available simulator sites.
Description This course comprises theoretical and practical training according to ATA Level IV on following engine types :
A300 B2/B4 GE CF6 and PW JT9,
A300-600 GE CF6 and PW4152,
A310 GE CF6 and PWJT9 and PW 4152,
A318/A319/320/321 CFM 56 and IAE V2500
A330 GE CF6-80 , RR TRENT700 , PW 4160
A340 CFM 56
The engine run-up training provides skills and experiences with starting and operating the engines and related
aircraft systems. It emphasizes recognition of normal and abnormal engine and systems operation and
provides skills for checking engine performance characteristics.
The theoretical training element of 8 hours covers exterior and interior engine inspections required prior to the
engine run-up, tests to be performed, engine limitations to be served and the necessary normal, abnormal,
emergency and safety procedures involved.
The practical training element of 4 hours functional training, for two trainees, uses adequate Full Flight
Simulators enabling them to learn the necessary procedures, apply the various checklists and confirm their
competence for task performance.
Continuous assessment is performed during the practical training.
Documentation • Cockpit Panel Drawings 1/2 scale
• Maintenance Practical Training Manual
• Engine Run-up Check-List
Course description A320 CFM or V2500
Engine Run-up Initial Training.doc
30/01/2009
WE QUALIFY!
PART-147 APPROVED TRAINING CENTER
19, rue Marcel ISSARTIER
Bât. M5 RDC – Station 57
CS 50008 - 33693 Mérignac Cedex - France
Phone : +33 (0)5 56 55 41 63
Fax : +33 (0)5 56 55 44 68
Site : www.sabenatechnicstraining.com
Email : training@sabenatechnics.com
SIREN 452 506 793 - VAT FR 97 452 506 793
R.C.S. Bordeaux 452 506 793
2 / 2
Course Syllabus
DAY ONE : THEORETICAL TRAINING
OTHER DAYS: FLIGHT SIMULATOR
TIME CHAPTER TIME CHAPTER
8H00 1– Run-up generality:
1.1 Safety precautions
1.2 Walk around
1.3 Hazardous areas
0H00 1– Briefing :
1.1 Safety precautions
1.2 Safety check
9H10 2 – A/C rewiew :
2.1 Cockpit
2.2 Systems
2.3 Engines
1H00 2 – Starting :
2.1 Cockpit preparation
2.2 APU start
2.3 Dry motoring
2.4 Wet motoring
2.5 Automatic start
2.6 Manual start
2.7 Shut Down
10H30 3 – Limitations, Environnement :
3.1 Operation limits
3.2 Radio-com
3.3 Environnement
3H00 3 – Operating :
3.1 Engine limits
3.2 Abnormal procedures
3.3 Engine test procedures
3.4 Emergency shut down
3.5 A/C leaving
11H30 4 – Normal Engine Operating Procedures :
4.1 Dry motoring
4.2 Wet motoring
5h10 4 – Debriefing :
4.1 Safety actions
4.2 Working team
4.3 Procedures follow up
4.4 Emergency behaviour
4.5 Approval assessment
12H00 Lunch
6H00 End
13H00 4 – Normal Engine Operating Procedures :
4.3 Engine automatic start
4.4 Engine manual start
13h40 5 – Emergency Procedures :
5.1 Abnormal operations
5.2 Engine fire
5.3 Engine tail fire
5.4 APU fire
5.5 Avionics smoke
5.6 Cargo smoke
15H00 6 – Engine Test Procedures :
6.1 Minimum idle check
6.2 Power assurance check
6.3 Vibration check
6.4 Acceleration check
16H00 End | 
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